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Northrop M2-F2

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M2-F2
General information
TypeLifting body technology demonstrator
National originUnited States
ManufacturerNorthrop
StatusRebuilt as M2-F3
Primary userNASA
Number built1
History
First flight12 July 1966
Retired10 May 1967
Developed fromNASA M2-F1
VariantsNorthrop M2-F3

The Northrop M2-F2 was a heavyweight lifting body based on studies at NASA's Ames and Langley research centers and built by the Northrop Corporation in 1966.

Development

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The success of Dryden's M2-F1 program led to NASA's development and construction of two heavyweight lifting bodies based on studies at NASA's Ames and Langley research centers—the M2-F2 and the HL-10, both built by the Northrop Corporation. The "M" refers to "manned" and "F" refers to "flight" version. "HL" comes from "horizontal landing" and 10 is for the tenth lifting body model to be investigated by Langley.

On March 23, 1966 the M2-F2 made its first captive flight—attached to the B-52 carrier aircraft throughout. The first free gliding flight of the M2-F2 was on July 12, 1966, piloted by Milton O. Thompson. He was dropped from the B-52 carrier aircraft's wing pylon at an altitude of 45,000 ft (14,000 m) and reached a speed of about 450 mph (720 km/h; 390 kn).

Operational history

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The crash site of the M2-F2

Before powered flights were undertaken, a series of glide flights were conducted. On May 10, 1967, the sixteenth and last glide flight ended in disaster as the vehicle slammed into the lake bed on landing. With test pilot Bruce Peterson at the controls, the M2-F2 suffered a pilot induced oscillation (PIO) as it neared the lake bed. At the core of this problem was the fact that the wings of the M2-F2 (essentially the body of the aircraft) produced considerably less roll authority than most aircraft. This resulted in less force available to the pilot to control the aircraft in roll. The vehicle rolled from side to side in flight as he tried to bring it under control. Peterson recovered, but then observed a rescue helicopter that seemed to pose a collision threat. Distracted, Peterson drifted in a crosswind to an unmarked area of the lake bed where it was very difficult to judge the height over the ground because of a lack of guidance (the markers provided on the lake bed runway).[1]

Peterson fired the landing rockets to provide additional lift, but he hit the lake bed before the landing gear was fully down and locked. The M2-F2 rolled over six times, coming to rest upside down. Pulled from the vehicle by Jay King and Joseph Huxman, Peterson was rushed to the base hospital, transferred to the March Air Force Base Hospital and then the UCLA Hospital. He recovered but lost vision in his right eye due to a staphylococcal infection.

Portions of M2-F2 footage including Peterson's spectacular crash landing were used for the 1973 television series The Six Million Dollar Man[2] though some shots during the opening credits of the series showed the later HL-10 model, during release from its carrier plane, a modified B-52.

Four pilots flew the M2-F2 on its 16 glide flights. They were Milton O. Thompson (five flights), Bruce Peterson (three flights), Don Sorlie (three flights) and Jerry Gentry (five flights).[citation needed]

NASA pilots and researchers realized the M2-F2 had lateral control problems, even though it had a stability augmentation control system. When the M2-F2 was rebuilt at Dryden and redesignated the M2-F3, it was modified with an additional third vertical fin—centered between the tip fins to improve control characteristics.

The M2-F2/F3 was the first of the heavyweight, entry-configuration lifting bodies. Its successful development as a research test vehicle answered many of the generic questions about these vehicles.

M2-F2 flights

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  • NASA M2-F2 - NASA 803, 16 unpowered flights
Vehicle
Flight # 		Date Pilot Mach Velocity
(km/h) 		Altitude
(meters) 		Duration Comments
M2-F2 #1 July 12, 1966 Thompson 0.646 727 13,716 00:03:37 First M2-F2 Flight. Unpowered glide. 320 km/h landing.
M2-F2 #2 July 19, 1966 Thompson 0.598 634 13,716 00:04:05 Unpowered glide. Determination of lateral stability control, longitudinal trim, vehicle performance and landing characteristics.
M2-F2 #3 August 12, 1966 Thompson 0.619 692 13,716 00:04:38 Unpowered glide. Determine effect of increasing Mach number, minimum damper requirements, testing of longitudinal and lateral stability and control.
M2-F2 #4 August 24, 1966 Thompson 0.676 718 13,716 00:04:01 Unpowered glide. Determine control damper requirements, lift-drag ratio, elevon response, flap effectiveness and longitudinal stability and control.
M2-F2 #5 September 2, 1966 Thompson 0.707 750 13,716 00:03:46 Unpowered glide. Evaluate 360 degree overhead approach, determine control damper-off handling qualities.
M2-F2 #6 September 15, 1966 Peterson 0.705 750 13,716 00:03:30 Unpowered glide. Pilot checkout.
M2-F2 #7 September 20, 1966 Sorlie 0.635 678 13,716 00:03:31 Unpowered glide. Pilot checkout.
M2-F2 #8 September 22, 1966 Peterson 0.661 702 13,716 00:03:53 Unpowered glide. Longitudinal and lateral stability and control with dampers.
M2-F2 #9 September 28, 1966 Sorlie 0.672 713 13,716 00:03:53 Unpowered glide. Complete pilot checkout and extend flight envelope.
M2-F2 #10 October 5, 1966 Sorlie 0.615 692 13,716 00:03:45 Unpowered glide. Explore lateral and longitudinal stability and control characteristics with dampers on and off.
M2-F2 #11 October 12, 1966 Gentry 0.662 702 13,716 00:03:54 Unpowered glide. Pilot checkout.
M2-F2 #12 October 26, 1966 Gentry 0.605 642 13,716 00:03:47 Unpowered glide. Obtain stability and control data at 7 and 11 degree attack angles and upper flap effectiveness.
M2-F2 #13 November 14, 1966 Gentry 0.681 716 13,716 00:04:21 Unpowered glide. Test stability and control, determine vehicle performance characteristics.
M2-F2 #14 November 21, 1966 Gentry 0.695 735 13,716 00:03:50 Unpowered glide. Test stability and control, determine vehicle performance characteristics.
M2-F2 #15 May 2, 1967 Gentry 0.623 661 13,716 00:03:51 Unpowered glide.
M2-F2 #16 May 10, 1967 Peterson 0.612 649 13,716 00:03:43 Unpowered glide
Crash landing[3]

Specifications (M2-F2)

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NASA M2-F2 Lifting body diagram
NASA M2-F2 Lifting body diagram

Data from [citation needed]

General characteristics

  • Crew: 1
  • Length: 22 ft 2 in (6.76 m)
  • Wingspan: 9 ft 8 in (2.95 m)
  • Height: 9 ft 6 in (2.90 m)
  • Wing area: 160 sq ft (15 m2)
  • Empty weight: 4,620 lb (2,096 kg)
  • Gross weight: 6,000 lb (2,722 kg)
  • Max takeoff weight: 7,485 lb (3,395 kg)
  • Powerplant: 1 × Reaction Motors XLR-11 liquid-fuelled rocket motor, 8,000 lbf (36 kN) thrust with four combustion chamber/nozzle assemblies

Performance

  • Maximum speed: 405 kn (466 mph, 750 km/h)
  • Maximum speed: Mach 0.707
  • Range: 8.6 nmi (9.9 mi, 15.9 km)
  • Service ceiling: 45,000 ft (14,000 m)
  • Wing loading: 43.2 lb/sq ft (211 kg/m2)
  • Thrust/weight: 1.3

See also

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Aircraft of comparable role, configuration, and era

References

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  1. ^ "1967 M2-F2 Crash at Edwards". Check-Six.com. Retrieved 14 April 2017.
  2. ^ Klingler, Dave (2012-09-06). "50 years to orbit: Dream Chaser's crazy Cold War backstory: The reusable mini-spaceplane is back from the dead—again—and prepping for space". Ars Technical. Retrieved 2012-09-07. The M2-F2 went on to star in the opening credits of "The Six Million Dollar Man,"
  3. ^ "1967 M2-F2 Crash at Edwards". Check-Six.com. Retrieved 14 April 2017.
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